Dual Chamber Combustor

ABSTRACT

Described herein is a combustor having a first burn chamber and a second burn chamber. The first burn chamber has a first burner and the second burn chamber has a second, separate burner. The first burn chamber is in fluid communication with the second burn chamber which allows particles or vapor to move from the first burn chamber to the second burn chamber. The first burn chamber is configured to perform a primary burn on particles or vapors that have been introduced into the first chamber and the second burn chamber is configured to perform a secondary burn on particles that have not been burned in the first chamber and move to the second burn chamber.

RELATED APPLICATIONS

This application is related to U.S. Provisional patent application Ser.No. ______, entitled “Environmental Condensing Apparatus”, filed on______. The aforementioned application is hereby incorporated byreference in its entirety.

TECHNICAL FIELD

The present disclosure generally relates to the field of combustors.

BACKGROUND

Vapor combustors may be used to destroy vapors and other harmfulparticles that may be present as a result of drilling and/or miningnatural resources. Typically, a combustor is used to burn some of thevapors prior to releasing the drilling byproducts into the atmosphere.Typically, combustors utilize a single burner to burn vapors as they areintroduced into the combustor. However, a single burner may not alwaysburn the vapors completely. Therefore the possibility remains thatharmful vapors may be released into the atmosphere.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a dual chamber combustor according to embodiments.

FIG. 2 shows the flow of vapors within the dual chamber combustor ofFIG. 1 according to embodiments.

FIG. 3 shows a combustor having a dual burn system according toembodiments.

FIG. 4 is a flow chart depicting a method for burning vapors accordingto embodiments.

DETAILED DESCRIPTION

This disclosure will now more fully describe exemplary embodiments withreference to the accompanying drawings, in which specific embodimentsare shown. Other aspects may be embodied in many different forms and theinclusion of specific embodiments in the disclosure should not beconstrued as limiting such aspects to the embodiments set forth herein.Rather, the embodiments depicted in the drawings are included to providea disclosure that is thorough and complete and which fully conveys theintended scope to those skilled in the art. When referring to thefigures, like structures and elements are shown throughout are indicatedwith like reference numerals.

Terminology

The terms and phrases as indicated in quotes (“ ”) in this section areintended to have the meaning ascribed to them in this Terminologysection applied to them throughout this document including the claimsunless clearly indicated otherwise in context. Further, as applicable,the stated definitions are to apply, regardless of the word or phrase'scase, to the singular and plural variations of the defined word orphrase.

The term “or” as used in this specification and the appended claims isnot meant to be exclusive rather the term is inclusive meaning “eitheror both”.

References in the specification to “one embodiment”, “an embodiment”, “apreferred embodiment”, “an alternative embodiment” and similar phrasesmean that a particular feature, structure, or characteristic describedin connection with the embodiment is included in at least an embodimentof the invention. The appearances of the phrase “in one embodiment” invarious places in the specification are not necessarily all meant torefer to the same embodiment.

The term “couple” or “coupled” as used in this specification and theappended claims refers to either an indirect or direct connectionbetween the identified elements, components or objects. Often the mannerof the coupling will be related specifically to the manner in which thetwo coupled elements interact.

Directional and/or relationary terms such as, but not limited to, left,right, nadir, apex, top, bottom, vertical, horizontal, back, front andlateral are relative to each other and are dependent on the specificorientation of an applicable element or article, and are usedaccordingly to aid in the description of the various embodiments and arenot necessarily intended to be construed as limiting.

The term “vapor” as used herein means any particle(s), vapors,combustible gas and any byproduct of mining or drilling for natural gasand other naturally occurring resource.

Described herein is a combustor having a first burn chamber and a secondburn chamber. The first burn chamber has a first burner and the secondburn chamber has a second, separate burner. The first burn chamber is influid communication with the second burn chamber which allows vapors tomove from the first burn chamber to the second burn chamber. The firstburn chamber is configured to perform a primary burn on the vapors thathave been introduced into the first chamber and the second burn chamberis configured to perform a secondary burn on the vapors that have notbeen burned in the first chamber and move to the second burn chamber.

Also described herein is a system for burning vapors. The systemincludes a primary burn module having a first burning apparatus disposedtherein. The first burning apparatus is configured to perform a primaryburn on vapors as the vapors are introduced into the system. The systemalso includes a secondary burn module having a second burning apparatusdisposed therein. The second burning apparatus is configured to performa secondary burn on the vapors after the vapors have moved from theprimary burn module into the secondary burn module. A cool down chamberdisposed between the first burn module and the second burn module and isconfigured to cool the vapors as the vapors pass from the primary burnmodule to the secondary burn module.

Still yet other embodiments provide a method for burning vapors in acombustor. The method includes introducing the vapors into at least oneburn chamber of a combustor. Once the vapors have been introduced, aprimary burn is performed on the vapors. A secondary burn is alsoperformed on the vapors. When both of the primary burn and the secondaryburn have been performed on the vapors, the vapor combustion byproductsare released into the atmosphere.

FIG. 1 shows a dual chamber combustor 100 according to embodiments. Thedual chamber combustor 100 is configured to perform at least two burnson vapors that are introduced into the combustor prior to releasing thevapors into the atmosphere. The vapors that are burned in the dualchamber combustor 100 include combustible hydrocarbons and othercombustible substances. The vapors are typically, but not necessarilyencountered or produced when drilling wells such as oil, gas or waterwells or during production from such wells. Vapors may also includesolid particles, liquid droplets, aerosols and gasses. The dual chambercombustor may be powered by any power source. Additionally, thecombustor may be powered by “green” energy sources. Examples include butare not limited to solar power, wind power, a twelve volt power sourceor any combination thereof. According to embodiments, a solar panel 104may be included on the dual chamber combustor 100 to provide power, orat least partially provide power, to the system.

The dual chamber combustor 100 includes a base portion 105 and a columnportion 107 in which the vapors are burned according to embodiments.Vapors are introduced into the dual chamber combustor 100 via a vaporinlet pipe 101. Prior to the vapors entering the combustor 100 via theinlet pipe 101, the vapors pass through a spark arrestor 103. The sparkarrestor is coupled to the inlet pipe 101 and is configured to prevent aflame from chasing down the inlet pipe 101 as vapors are introduced intothe dual chamber combustor 100. Embodiments provide that the sparkarrestor 103 is configured in a vertical position. Other embodimentsprovide that at least a portion of the vapor inlet pipe 101 isconfigured to have at least a two percent slope. Therefore, if anyvapors condense into a liquid, the liquid is able to drain out of thesystem. Other embodiments provide that the spark arrestor 103 may bedisposed in a horizontal position. When in the horizontal position, atleast a portion of the inlet pipe 101 that is coupled to the sparkarrestor has at least a two percent drop.

In embodiments, the base portion 105 and the column portion 107 arecoupled together to form a single unit. When coupled together, theheight of the dual chamber combustor 100 is approximately 18 feet.However, it is anticipated that the height may be adjusted based on thelocation and/or volume of vapor that will be burned in the combustor.

Although the dual chamber combustor 100 functions as a single unit,various components of the dual chamber combustor 100 may be removed,separated and operated independently. For example, the column portion107 may be removed from the base portion 105 for repair and replacementof components. Furthermore, the column 107 itself, as well as variouscomponents of the column 107 may be separated and removed. Such aconfiguration may enable a user of the dual chamber combustor 100 tomore easily repair and replace various components of the dual chambercombustor 100. It is also contemplated that although each of the variouscomponents of the dual chamber combustor are configured to worksimultaneously, or substantially simultaneously, with the other, eachcomponent of the dual chamber combustor 100 may function independentlyfrom each of the other components.

According to embodiments the base portion 105 of the dual chambercombustor 100 is constructed of standard sheet metal. However othermaterials or combination of materials may be used in the construction ofthe base portion 105 and/or the column portion 107. The dimensions ofthe base portion 105 are approximately 6′×4′×3′ although it iscontemplated that the base portion 105 may be constructed having variousother dimensions than those explicitly stated herein.

The base portion 105 includes at least one air intake mechanism 109disposed therein. According to embodiments, the air intake mechanism mayalso function as a flame arrestor. Although one air intake mechanism 109is shown in FIG. 1, it is possible that multiple air intake mechanismsmay be disposed on the base portion 105 of the dual chamber combustor100. According to embodiments, the air intake mechanism 109 is a 750,000BTU intake mechanism. Although a 750,000 BTU intake mechanism isspecifically disclosed, it is contemplated that various other intakemechanisms having various power requirements and outputs may be used. Inembodiments where multiple intake mechanisms are used, it iscontemplated that each intake mechanism may have equivalent BTUs. Otherembodiments provide that multiple intake mechanisms having differentBTUs may be used in combination.

The dual chamber combustor 100 also includes a column portion 107. Inembodiments, a flange 102 may be disposed on a lower portion of thecolumn portion 107. The flange 102 may be used to secure and separatethe column portion 107 of the combustor 100 from the base portion 105 ofthe combustor 100.

Embodiments provide that the column portion 107 includes a primary burnchamber 115, a cool down chamber 116, and a secondary burn chamber 117.The primary burn chamber 115 is in fluid communication with, via thecool down chamber 116, the secondary burn chamber 117. A flange 118couples the primary burn chamber 115, portions of the cool down chamber116, and the secondary burn chamber 117 together. The coupling of eachsection allows the vapors to flow from the primary burn chamber 115 tothe secondary burn chamber 117.

Embodiments provide that the primary burn chamber 115 is constructed often inch diameter schedule-twenty pipe. However, it is also contemplatedthat various other pipe sizes and schedules may be used. According toembodiments, at least a portion of the primary burn chamber 115 iscontained within the base portion 105 of the dual burn combustor 100.Such embodiments may permit a user access to various components that arecontained within the primary burn chamber, such as for example, aprimary burner, and/or pilot light, for maintenance and repair purposes.

In embodiments, a pilot light 120 and burner 122 are contained within alower portion of the primary burn chamber 115. The pilot light 120 andburner 122 is supplied with natural gas, or other combustible materialor vapor, through a standard natural gas line. The natural gas may besupplied from an on-site source, such as for example, a source that iscurrently being mined or drilled. Alternatively, the natural gas may besupplied from a tank or other portable source. According to embodiments,the pilot light and burner is a 750,000 BTU burner although other typesand strengths of burners may be used. The pilot light 120 and burner 122are configured to perform a primary burn on vapors as the vapors areintroduced into the primary burn chamber 115 of the dual burn combustor100 by the inlet pipe 101 and the spark arrestor 103 combination. It iscontemplated that an electronic ignition switch may be used in lieu of,or in combination with the pilot light.

The dual chamber combustor 100 also includes a sight glass 125 disposedon the primary burn chamber 115 according to embodiments. The sightglass 125 is positioned near the pilot light 120 and provides means bywhich a user may safely look into the primary burn chamber 115 todetermine whether the pilot light 120 is burning. A thermostat and/orthermometer (not shown) may also be disposed on a portion of the primaryburn chamber 115 to track and control the temperature within the primaryburn chamber 115. The thermostat may be powered by power source, suchas, but not limited to a generator, a battery, such as a twelve voltbattery, solar power, wind power or a combination thereof.

A cool down chamber 116 is disposed between the primary burn chamber 115and the secondary burn chamber 117. According to embodiments, the cooldown chamber 116 has a smaller diameter than the primary burn chamber115 and the secondary burn chamber 117. Embodiments provide that thecool down chamber is comprised of six inch diameter schedule twenty pipeand measures approximately twelve inches from A-A′ and approximately 18inches from B-B′. Although specific dimensions of the height and widthof pipe used for the cool down chamber 116 are mentioned, it iscontemplated that the cool down chamber 116 may have differing heightsand be constructed of pipe having various diameters and thickness. Forexample, the cool down chamber may be twelve inches in height and beconstructed of 9 inch diameter pipe.

The purpose of the cool down chamber 116 is to assist in cooling vaporsas the vapors pass from the primary burn chamber 115, where a primaryburn on the vapors was performed, to the secondary burn chamber 117,where a secondary burn on the vapors is performed. Because the cool downchamber 116 is narrower than the primary burn chamber 115, as vaporsattempt to enter the cool down chamber the cooler vapors are forced backdown the side and into the center of the primary burn chamber 115 andburned again in the primary burn chamber. Additionally, as the vaporsenter the narrower cool down chamber, the hotter, inner vapors arecombined with the cooler outer vapors cooler vapors of the vapor streamthereby cooling the overall temperature of the vapors.

The dual chamber combustor 100 also includes a secondary burn chamber117. According to embodiments, the secondary burn chamber 117 comprisesten inch diameter schedule-twenty pipe and measures approximately 18inches from section C to C′. Although specific dimensions have beendisclosed, it is contemplated that other dimensions may be used for thesecondary burn chamber 117.

The secondary burn chamber 117 includes a secondary pilot light andsecondary burner 130. The secondary pilot light 130 and secondary burner133 are fed natural gas that is provided either on site or provided byother means, such as for example a refillable tank, container and thelike. According to embodiments, the pilot 130 and secondary burner 133is a 125,000 BTU burner, although it is contemplated that other burnersmay be used. Alternative embodiments provide that an electronic ignitionswitch may be used, in lieu of, or in combination with a standard pilotlight.

The secondary burner 133 is disposed within the secondary burn chamber117 in such a position that as vapors pass from the cool down chamber116 to the secondary burn chamber 117, that the vapors come into contactwith the flame of the burner where a secondary burn is performed.According to embodiments, the secondary burner may be positioned atapproximately a forty-five degree angle with respect to the verticalpositioning of the secondary burn chamber. Alternatively, the secondaryburner may be horizontally disposed within the secondary burn chamber117. A flame shield 135 and a heat deflector 137 may also be disposedwithin the secondary burn chamber 117. The flame shield 135 ispositioned within the secondary burn chamber 117 so as to prevent theflame from the secondary burner 130 from coming into contact with anouter wall of the secondary burn chamber 117. When heated, the flameshield 135 may also be used to burn vapors as the vapors come intocontact with the flame shield 135. For example, if the burn shield hasbeen heated as a result of coming into contact with the secondary burner133, vapors may be burned as the vapor comes into contact with the flameshield 135.

According to embodiments, the flame shield 135 is positioned at aforty-five degree angle with respect to the vertical positioning ofsecondary burn chamber 117. The angle of the flame shield 135 causes thevapors to circulate within the secondary burn chamber 117 prior to beingreleased into the atmosphere via the exhaust pipe 160. Circulation ofthe vapors within the secondary burn chamber 117 may cause the vapors tocome into contact with the secondary burner 133 and/or a heated flameshield 135 multiple times which may increases the probability thatundesirable vapors will be substantially completely burned. Otherembodiments provide that the flame shield is placed at other varyingangles. Still yet other embodiments provide that the flame shield 135 isadjustable and may be moved between desired angles using an adjustmentmechanism (not shown). The flame shield 135 is also removable andreplaceable. Such a configuration may allow for easier maintenance andrepair.

The secondary burn chamber 117 also includes a secondary flame arrestor140 disposed thereon. The secondary flame arrestor 140 comprises a125,000 BTU intake according to embodiments. However it is contemplatedthat various flame arrestors having varying strengths may be used. Asecondary air intake (not shown) can also be included on the secondaryburn chamber 117.

A temperature controller 150 and a high temperature shutdown mechanism155 are disposed on the secondary burn chamber to control thetemperature of the secondary burn chamber. The temperature controller150 may be powered by a power source. Examples include, but are notlimited to “green” power sources such as a twelve volt power source,solar power, wind energy or a combination thereof. A thermometer (notshown) may also be disposed on the secondary burn chamber 117 andconfigured to track the temperature within secondary burn chamber 117.

According to embodiments, an exhaust pipe 160 is disposed on an upperportion of the secondary burn chamber 117. The exhaust pipe 160 istypically comprised of eight inch pipe and measures approximately 8 feetin height. However, it is contemplated the height, width and thicknessof pipe used for the exhaust pipe 160 may vary. A flange 165 may bedisposed on the exhaust pipe 160 which enables the exhaust pipe 160 tobe removed from the secondary burn chamber 117. Such embodiments mayprovide means whereby a user may inspect the secondary burn chamber 117and its components as well as repair and/or replace the componentstherein.

FIGS. 2-4 illustrate various aspects and features of a dual chambercombustor such as the dual chamber combustor 100 of FIG. 1 according toembodiments. FIGS. 2-4 also show components that were first describedwith respect to FIG. 1 and therefore the description of FIGS. 2-4 mayrefer to at least one component described in FIG. 1. However, anyreferences to components of FIG. 1 are for descriptive purposes only.

FIG. 2 shows the flow of vapors 210 within a dual chamber combustor,such as for example, the dual chamber combustor 100 of FIG. 1 accordingto embodiments. In FIG. 2, the flow of vapors 210 is represented bydirectional arrows. As shown in FIG. 2, the vapors 210 are introducedinto the dual chamber combustor 100 via a vapor inlet pipe 101 (FIG. 1).The vapor inlet pipe 101 releases the vapors into the primary burnchamber 117 where a primary burn is performed on the vapors by theprimary burner 123. Vapors that are not completely burned in the primaryburn, along with any combustibles that remain as a byproduct of thevapors being burned, travel in an upward direction toward the secondaryburn chamber 119 as indicated by the directional arrows.

Prior to entering the secondary burn chamber 117, the vapors passthrough a cool down chamber, such as cool down chamber 116 (FIG. 1).Because the cool down chamber 116 is narrower than the primary burnchamber 115, cooler vapors on the outside of the vapor stream eithercombine with the hotter vapors in the inner vapor stream or the coolervapors are forced down the side of the primary burn chamber 115 and areburned. When the vapors exit the cool down chamber 116, the vaporsexpand which causes the vapors 210 to cool.

As the vapors 210 continue to travel in an upward direction into thesecondary burn chamber 117, a secondary burn is performed on theremaining vapors 210 by the secondary burner 130 (FIG. 1). As describedabove, a flame shield 135 (FIG. 1) may be disposed in the secondary burnchamber 117. The flame shield is positioned at a predetermined anglewithin the chamber. The flame shield 135 may be used to shield the wallof the secondary burn chamber 117 from coming into direct contact withthe flame of the secondary burner 130. When hot, the flame shield 135may also act as an incinerator and burn vapors 210 as the vapors comeinto contact with the flame shield 135. The flame shield 135 may alsocause the circulation or rolling of the vapors 210 within the secondaryburn chamber 117. Circulation or rolling of the vapors 210 within thesecondary burn chamber 117 causes vapors 210 that were not entirelyburned in the primary burn chamber 115 and/or were not burned uponentrance into the secondary burn chamber 117 to pass by the secondaryburner at least a second time in an attempt to completely burn thevapors 210.

After circulation, the vapors 210, are released into the atmosphere viaan exhaust pipe, such as exhaust pipe 160 (FIG. 1). As described above,the exhaust pipe 160 is constructed of pipe that is smaller than thepipe of the secondary burn chamber 117. Introducing the remainingvapors, if any, along with the byproduct of the burned vapors, into asmaller pipe will increase the velocity at which the vapors travel in anupward direction into the atmosphere. In embodiments, the system usesnatural gas for the burners, is powered by a power source that mayinclude at least one of, a rechargeable twelve volt battery source,solar power, wind power, or a combination thereof, the system may bemore environmentally friendly combustors without the features describedherein.

FIG. 3 shows a combustor 300 having a dual burn system according toembodiments. The combustor 300 includes a base portion 305 and a columnportion 307. The base portion includes at least one flame arrestor andair intake mechanism 309. According to embodiments, the flame arrestorand air intake mechanism may be function as a single unit. As will beexplained in more detail below, the column portion 307 includes at leasttwo burners. A first burner 323 is disposed on a lower portion of thechamber portion 307 and a second burner 333 is disposed on an upper,narrower portion of the chamber portion 307. The column portion 307 alsoincludes a second air intake mechanism 345 disposed near the secondburner 333. Embodiments provide that the second air intake mechanism maybe combined with or function as a flame arrestor. As discussed, thecolumn portion 107 has two sections according to embodiments. The lowerportion 315 of the column portion 107 is constructed of ten inchschedule-twenty pipe, while the upper portion 317 of the column portion107 is constructed of pipe having a smaller diameter than the lowerportion 315.

Vapors are introduced into the combustor 300 via a vapor inlet pipe 301.Prior to entering the combustor 300, the vapors pass through a sparkarrestor 303. According to embodiments, the spark arrestor 303 isconfigured vertically. It is also contemplated that at least a portionof the vapor inlet pipe 301, is configured to have at least a twopercent drop prior to being coupled to the spark arrestor 303. The dropallows draining of any liquids that have formed due to the condensing ofvapors.

As the vapors are introduced into the lower portion 315 of the columnportion 307 of the combustor 300, the vapors are burned by a firstburner 323. The first burner is situated near a pilot light 320 and boththe first burner 323 and the pilot light 320 are configured to burnnatural gas. However, it is contemplated that other combustible fluidsmay be used.

Embodiments provide that a thermometer 321 is disposed on a lowerportion 315 of the column portion 307 for use in monitoring thetemperature within the lower portion 315 of the column portion 307. Asight glass 325 may also be positioned on the lower portion 315 of thecolumn portion 307. The sight glass 325 may be used to view the flameand/or the pilot light 320.

Once the vapors have been burned by the first burner 323, the vaporstravel in an upward direction toward the second burner 333 that ispositioned at the base of the upper portion 317 of the column portion307 of the combustor 300. According to embodiments, a flame arrestor 335is positioned near the second burner and pilot light 330 for increasedsafety. As the vapors enter the upper portion 317, the second burner 333performs a second burn on the vapors. The remaining vapors and theresidual from the first burn and the second burn travels in an upwarddirection, with increased velocity due to the narrowing of the upperportion, and are released into the atmosphere.

The combustor 300 also includes a twelve volt thermostat 350 positionedon the upper portion 317 of the column portion 307 as well as athermometer 355 to control and monitor the temperature in the upperportion 317 of the column portion 307 of the combustor 300.

FIG. 4 is a flow chart depicting a method 400 for burning vapors in acombustor according to embodiments. Step 410 provides that vapors areintroduced into the combustor, such as, for example the dual chambercombustor 100 (FIG. 1). As previously explained, the vapors may beintroduced into the combustor via an inlet pipe, a spark arrestor, or acombination thereof.

When the vapors have been introduced into the combustor, flow proceedsto step 420 in which a primary burn is performed on the vapors.According to embodiments, the primary burn on the vapors is performed bya primary burner disposed in a primary burn chamber, such as forexample, primary burn chamber 115 (FIG. 1).

Step 430 provides that the vapors are cooled. According to embodiments,the vapors are cooled by combining cooler vapors outer vapors of a vaporstream with hotter inner vapors of the vapor stream. This isaccomplished by introducing the vapors into a cool down chamber, suchas, for example, cool down chamber 116 (FIG. 1). Embodiments providethat the diameter of the cool down chamber is smaller than the diameterof the primary burn chamber. As the vapors enter the cool down chamberthe cooler vapors are combined with the hotter vapors, therebydecreasing the overall temperature of the vapors as they pass throughthe chamber. In addition, cooler vapors that are not combined with thehotter vapors are forced down the side of the primary burn chamber wherethey may be burned and forced upward once again. Upon exiting the cooldown chamber, the vapors are allowed to expand which causes the vaporsto cool.

Step 440 provides that a secondary burn is performed on the vapors.According to embodiments, the secondary burn is performed by a secondaryburner in a secondary burn chamber, such as, for example, secondary burnchamber 117 (FIG. 1). While in the secondary burn chamber, the vaporsmay be circulated so as to cause the vapors to come into contact withthe secondary burner and/or a heated flame shield disposed therein,multiple times. The circulation may cause more of the vapors to becompletely burned.

After the secondary burn and circulation, the remaining vapors, and thebyproduct of the burned vapors, are released into the atmosphere in step450. According to embodiments, the vapors are funneled through anexhaust pipe that is coupled to a top portion of the secondary burnchamber.

Although illustrative embodiments of the invention have been describedin detail herein with reference to the accompanying drawings, it is tobe understood that the invention is not limited to those preciseembodiments. As such, many modifications and variations will be apparentto practitioners skilled in this art. Accordingly, it is intended thatthe scope of the invention be defined by the following claims and theirequivalents. Furthermore, it is contemplated that a particular featuredescribed either individually or as part of an embodiment can becombined with other individually described features, or parts of otherembodiments, even if the other features and embodiments make nomentioned of the particular feature. Thus, the absence of describingcombinations should not preclude the inventor from claiming rights tosuch combinations.

1. A combustor comprising: a first burn chamber having a first burner;and a second burn chamber having a second burner, wherein the secondburn chamber is in fluid communication with the first burn chamber, andwherein the second burn chamber is configured to perform a secondaryburn on combustibles that have not been burned in the first burn chamberand move from the first burn chamber to the second burn chamber.
 2. Thecombustor of claim 1, further comprising a cool down chamber positionedbetween the first burn chamber and the second burn chamber.
 3. Thecombustor of claim 2, wherein the cool down chamber has a first diameterthat is smaller than a diameter of at least one of the first burnchamber and the second burn chamber.
 4. The combustor of claim 1,further comprising a flame shield contained within the secondary burnchamber.
 5. The combustor of claim 4, wherein an angle of the flameshield is adjustable.
 6. The combustor of claim 1, further comprising atleast one flame arrestor, wherein the at least one flame arrestorincludes at least one air intake mechanism.
 7. The combustor of claim 1,further comprising an exhaust funnel configured to expel the vapors fromthe combustor.
 8. The combustor of claim 1, further comprising at leastone power source, wherein the at least one power source is selected froma group consisting of (i) a solar panel source, (ii) a twelve voltbattery source, and (iii) a wind power source.
 9. A system for burningvapors, the system comprising: a primary burn module having a firstburning apparatus disposed therein, wherein the first burning apparatusis configured to perform a primary burn on vapors as the vapors areintroduced into the system; a secondary burn module having a secondburning apparatus disposed therein, wherein the second burning apparatusis configured to perform a secondary burn on the vapors after the vaporshave moved from the primary burn module into the secondary burn module;and a cool down chamber disposed between the first burn module and thesecond burn module, wherein the cool down chamber is configured to coolthe vapors as the vapors pass from the primary burn module to thesecondary burn module.
 10. The system of claim 9, wherein each of thefirst burn module and the second burn module have a first diameter andwherein the cool down chamber has second diameter that is different thanthe diameter of the first burn module and the second burn module. 11.The system of claim 9, further comprising a plurality of flamearrestors, wherein a first one of the plurality of flame arrestors isadapted for the first burn module and wherein a second one of theplurality of flame arrestors is adapted for the second burn module. 12.The system of claim 9, further comprising a plurality of air intakevalves, wherein at least a first one of the plurality of air intakevalves is adapted for the first burn module and wherein at least asecond one of the plurality of air intake valves is adapted for thesecond burn module.
 13. The system of claim 9, further comprising aspark arrestor.
 14. The system of claim 13, wherein the spark arrestoris disposed in a vertical position.
 15. The system of claim 9, furthercomprising a heat shield moveably disposed within the second burnmodule.
 16. The system of claim 9, further comprising a power source,wherein the power source is at least one of (i) a solar power source,(ii) a wind power source, and (iii) a twelve volt battery power source.17. The system of claim 9 further comprising an exhaust, wherein theexhaust is configured to release vapors into the atmosphere after thevapors have traveled through the primary burn module and the secondaryburn module.
 18. A method for burning vapors, the method comprising:introducing the vapors into at least one burn chamber; performing aprimary burn on the vapors; cooling the vapors; performing a secondaryburn on the vapors; and releasing the vapors into the atmosphere whenthe vapors have been burned by the primary burn and the secondary burn.19. The method of claim 18, wherein cooling the vapors comprisesintroducing the vapors into a cool down chamber, wherein the cool downchamber has a smaller diameter than a first chamber where the primaryburn is performed.
 20. The method of claim 18, further comprisingcirculating the vapors in a chamber during at least one of the primaryburn or the secondary burn.